The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 05, 2019

Filed:

Feb. 18, 2015
Applicant:

Siemens Aktiengesellschaft, München, DE;

Inventors:

Ramesh Subramanian, Oviedo, FL (US);

Neil Hitchman, Charlotte, NC (US);

Dimitrios Zois, Berlin, DE;

Jonathan E. Shipper, Jr., Lake Mary, FL (US);

Cora Schillig, Charlotte, FL (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); F01D 5/18 (2006.01); F01D 9/02 (2006.01); C23C 4/04 (2006.01); C23C 4/12 (2016.01); F01D 11/12 (2006.01); F01D 11/08 (2006.01); F01D 9/04 (2006.01); F01D 25/12 (2006.01);
U.S. Cl.
CPC ...
F01D 11/122 (2013.01); C23C 4/04 (2013.01); C23C 4/12 (2013.01); F01D 5/18 (2013.01); F01D 5/187 (2013.01); F01D 5/288 (2013.01); F01D 9/02 (2013.01); F01D 9/041 (2013.01); F01D 11/08 (2013.01); F01D 25/12 (2013.01); F05D 2220/31 (2013.01); F05D 2220/32 (2013.01); F05D 2230/311 (2013.01); F05D 2230/312 (2013.01); F05D 2230/90 (2013.01); F05D 2240/11 (2013.01); F05D 2250/00 (2013.01); F05D 2250/141 (2013.01); F05D 2250/18 (2013.01); F05D 2250/181 (2013.01); F05D 2250/182 (2013.01); F05D 2250/185 (2013.01); F05D 2250/23 (2013.01); F05D 2250/28 (2013.01); F05D 2250/294 (2013.01); F05D 2260/202 (2013.01); F05D 2260/231 (2013.01); F05D 2260/941 (2013.01); F05D 2300/10 (2013.01); F05D 2300/21 (2013.01); F05D 2300/5023 (2013.01); F05D 2300/516 (2013.01); F05D 2300/611 (2013.01);
Abstract

Engineered groove features (EGFs) are formed within thermal barrier coatings (TBCs) of turbine engine components. The EGFs are advantageously aligned with likely stress zones within the TBC or randomly aligned in a convenient two-dimensional or polygonal planform pattern on the TBC surface and into the TBC layer. The EGFs localize thermal stress- or foreign object damage (FOD)-induced crack propagation within the TBC that might otherwise allow excessive TBC spallation and subsequent thermal exposure damage to the turbine component underlying substrate. Propagation of a crack is arrested when it reaches an EGF, so that it does not cross over the groove to otherwise undamaged zones of the TBC layer. In some embodiments, the EGFs are combined with engineered surface features (ESFs) that are formed in the component substrate or within intermediate layers applied between the substrate and the TBC.


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